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DE3665764D1 - Liner construction - Google Patents

Liner construction

Info

Publication number
DE3665764D1
DE3665764D1 DE8686630109T DE3665764T DE3665764D1 DE 3665764 D1 DE3665764 D1 DE 3665764D1 DE 8686630109 T DE8686630109 T DE 8686630109T DE 3665764 T DE3665764 T DE 3665764T DE 3665764 D1 DE3665764 D1 DE 3665764D1
Authority
DE
Germany
Prior art keywords
liner construction
liner
construction
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DE8686630109T
Other languages
German (de)
Inventor
Lawrence Harold Drobny
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE3665764D1 publication Critical patent/DE3665764D1/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/40—Clamping arrangements where clamping parts are received in recesses of elements to be connected
    • F16B2200/403—Threaded clamping parts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Window Of Vehicle (AREA)
  • Seal Device For Vehicle (AREA)
  • Control And Other Processes For Unpacking Of Materials (AREA)
DE8686630109T 1985-07-03 1986-07-02 Liner construction Expired DE3665764D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/751,753 US4748806A (en) 1985-07-03 1985-07-03 Attachment means

Publications (1)

Publication Number Publication Date
DE3665764D1 true DE3665764D1 (en) 1989-10-26

Family

ID=25023340

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686630109T Expired DE3665764D1 (en) 1985-07-03 1986-07-02 Liner construction

Country Status (4)

Country Link
US (1) US4748806A (en)
EP (1) EP0216721B1 (en)
JP (1) JPH0819927B2 (en)
DE (1) DE3665764D1 (en)

Families Citing this family (47)

* Cited by examiner, † Cited by third party
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FR2599821B1 (en) * 1986-06-04 1988-09-02 Snecma COMBUSTION CHAMBER FOR TURBOMACHINES WITH MIXING HOLES PROVIDING THE POSITIONING OF THE HOT WALL ON THE COLD WALL
US4848089A (en) * 1988-02-18 1989-07-18 Avco Corporation Combustor attachment device
JP2680029B2 (en) * 1988-04-08 1997-11-19 株式会社日立製作所 Thermosetting resin composition
US4920742A (en) * 1988-05-31 1990-05-01 General Electric Company Heat shield for gas turbine engine frame
US4971497A (en) * 1990-03-02 1990-11-20 The United States Of America As Represented By The Secretary Of The Air Force Fastener system
US5113660A (en) * 1990-06-27 1992-05-19 The United States Of America As Represented By The Secretary Of The Air Force High temperature combustor liner
US5105625A (en) * 1990-11-23 1992-04-21 General Motors Corporation Mounting for a ceramic scroll in a gas turbine machine
US5144793A (en) * 1990-12-24 1992-09-08 United Technologies Corporation Integrated connector/airtube for a turbomachine's combustion chamber walls
JP2838446B2 (en) * 1991-02-22 1998-12-16 株式会社クボタ Engine warm-up promotion device for engine heating system
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
US5129447A (en) * 1991-05-20 1992-07-14 United Technologies Corporation Cooled bolting arrangement
US5216886A (en) * 1991-08-14 1993-06-08 The United States Of America As Represented By The Secretary Of The Air Force Segmented cell wall liner for a combustion chamber
US5186006A (en) * 1992-03-19 1993-02-16 General Motors Corporation Mounting for ceramic scroll
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly
FR2708086B1 (en) * 1993-06-30 1995-09-01 Snecma Sectorized tubular structure working on implosion.
US5592814A (en) * 1994-12-21 1997-01-14 United Technologies Corporation Attaching brittle composite structures in gas turbine engines for resiliently accommodating thermal expansion
DE19502730A1 (en) * 1995-01-28 1996-08-01 Abb Management Ag Ceramic lining
DE19623300A1 (en) * 1996-06-11 1997-12-18 Siemens Ag Heat shield arrangement, in particular for structural parts of gas turbine plants, with a layered structure
US6351949B1 (en) * 1999-09-03 2002-03-05 Allison Advanced Development Company Interchangeable combustor chute
DE10114619B4 (en) * 2000-03-27 2006-07-27 Cummins Inc., Columbus Ventilating fastening element
US6497105B1 (en) 2001-06-04 2002-12-24 Pratt & Whitney Canada Corp. Low cost combustor burner collar
US7146815B2 (en) * 2003-07-31 2006-12-12 United Technologies Corporation Combustor
US7134286B2 (en) * 2004-08-24 2006-11-14 Pratt & Whitney Canada Corp. Gas turbine floating collar arrangement
US7140189B2 (en) * 2004-08-24 2006-11-28 Pratt & Whitney Canada Corp. Gas turbine floating collar
EP1712840A1 (en) * 2005-04-13 2006-10-18 Siemens Aktiengesellschaft Heat shield assembly with fixation bolt
US7721522B2 (en) * 2006-01-05 2010-05-25 United Technologies Corporation Torque load transfer attachment hardware
US7926280B2 (en) * 2007-05-16 2011-04-19 Pratt & Whitney Canada Corp. Interface between a combustor and fuel nozzle
FR2923528B1 (en) * 2007-11-13 2009-12-11 Snecma TURBINE OR COMPRESSOR STAGE OF A TURBOREACTOR
JP4863020B2 (en) * 2008-02-25 2012-01-25 井関農機株式会社 Combine
JP4863019B2 (en) * 2008-02-25 2012-01-25 井関農機株式会社 Combine
JP4863018B2 (en) * 2008-02-25 2012-01-25 井関農機株式会社 Combine
JP4775458B2 (en) * 2009-02-27 2011-09-21 井関農機株式会社 Combine
US8590313B2 (en) * 2008-07-30 2013-11-26 Rolls-Royce Corporation Precision counter-swirl combustor
ES2551161T3 (en) * 2008-11-28 2015-11-16 Acs Industries, Inc. Wire mesh rivet
US10107497B2 (en) 2012-10-04 2018-10-23 United Technologies Corporation Gas turbine engine combustor liner
GB201222311D0 (en) * 2012-12-12 2013-01-23 Rolls Royce Plc A combusiton chamber
US9447700B2 (en) * 2013-02-19 2016-09-20 United Technologies Corporation Thermally free hanger with length adjustment feature
GB201303057D0 (en) * 2013-02-21 2013-04-03 Rolls Royce Plc A combustion chamber
GB201317006D0 (en) * 2013-09-25 2013-11-06 Rolls Royce Plc Component for attaching to a wall
WO2015105654A1 (en) 2014-01-08 2015-07-16 United Technologies Corporation Clamping seal for jet engine mid-turbine frame
US9890953B2 (en) * 2014-01-10 2018-02-13 United Technologies Corporation Attachment of ceramic matrix composite panel to liner
EP3099903B1 (en) * 2014-01-28 2020-04-22 United Technologies Corporation Seal for jet engine mid-turbine frame
US10634349B2 (en) * 2015-08-24 2020-04-28 General Electric Company Wear pad system for turbine combustion systems and method for coupling wear pad into turbine combustion system
CN108425931B (en) * 2018-04-24 2021-03-02 奇瑞汽车股份有限公司 Automobile number plate fixing nut seat and number plate fixing structure and automobile with same
US11435078B2 (en) * 2018-12-20 2022-09-06 Pratt & Whitney Canada Corp. Stand-off device for double-skin combustor liner
JP2023183452A (en) * 2022-06-16 2023-12-28 川崎重工業株式会社 gas turbine combustor
US11788491B1 (en) 2022-07-13 2023-10-17 General Electric Company Systems and methods for attachment of materials having different thermal expansion coefficients

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2334263A (en) * 1941-06-03 1943-11-16 Metal Textile Corp Foraminous body and method of producing the same
GB701099A (en) * 1950-05-22 1953-12-16 Lucas Ltd Joseph Improvements to combustion chambers
US2869858A (en) * 1956-08-01 1959-01-20 Metal Textile Corp Vibration and shock absorptive cushion element
FR1214261A (en) * 1957-10-28 1960-04-07 Canadian Patents Dev Gas turbojet channel wall
FR1228407A (en) * 1958-03-25 1960-08-29 Zd Y V I Flame tube for combustion chambers of gas turbine installations
US3073557A (en) * 1961-10-10 1963-01-15 Robinson Technical Products In Shock and vibration isolating mountings for aircraft engines and the like
GB1176791A (en) * 1965-10-06 1970-01-07 Delaney Gallay Ltd Improvements in and relating to Vibration or Shock Isolation Units.
US3390709A (en) * 1965-11-29 1968-07-02 Lord Corp Resilient mounting
GB1183143A (en) * 1968-01-17 1970-03-04 Rolls Royce Improvements in or relating to the Mounting of a Liner in a Duct
SE314558B (en) * 1968-10-28 1969-09-08 Stal Laval Turbin Ab
US3932056A (en) * 1973-09-27 1976-01-13 Barry Wright Corporation Vane damping
GB1487064A (en) * 1974-08-23 1977-09-28 Rolls Royce Wall structure for hot fluid streams
US4312599A (en) * 1979-10-22 1982-01-26 General Electric Company High temperature article, article retainer, and cushion
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
GB2087065B (en) * 1980-11-08 1984-11-07 Rolls Royce Wall structure for a combustion chamber
JPH0130254Y2 (en) * 1981-03-20 1989-09-14
US4512159A (en) * 1984-04-02 1985-04-23 United Technologies Corporation Clip attachment

Also Published As

Publication number Publication date
JPS6224016A (en) 1987-02-02
EP0216721B1 (en) 1989-09-20
JPH0819927B2 (en) 1996-03-04
US4748806A (en) 1988-06-07
EP0216721A1 (en) 1987-04-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee